EGYPTSAT A, 44047
Orbit data source: Space-Track
EGYPTSAT A, 44047 is a payload satellite owned by EgSA (EG) in SSO that was launched on Thu, 21 Feb 2019 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44047 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / EGYPRelated business
Manufacturer
Yuzhnoe
Mission
Operational Civil Imaging
Bus & Motor
EGYPTSAT, Unknown motor
Mass
~1,050 kg wet, ~1,050 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan + 1 Ant, 1.0 m
Radar Cross Section
0.867 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 EGYPTSAT A
1 44047U 19008A 25294.66758314 .00001202 00000-0 19813-3 0 9999
2 44047 98.0062 357.9433 0000990 82.6299 277.5020 14.72272374358147Epoch: 2025-10-21T16:01Z
TLE epoch observation values (Epoch: 2025-10-21T16:01:19.183Z)
Latitude
-0.0001°
Longitude
87.26114°
Altitude
656.74 km
Speed
7.529 km/s
True Right ascension
23h 51m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:54:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.575 km
Perigee altitude
650.183 km
Semi-major axis
7,029.016 km
Eccentricity
0.0001
Inclination
98.0062°
RAAN
357.9433°
Arg. of periapsis
82.6299°
True anomaly
277.49075°
Mean anomaly
277.502°
Eccentric anomaly
277.49638°
Mean motion
3.683 °/min
Orbital period
97.75 mins
BSTAR
0.00019813
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Other satellites on launch #8 in the year 2019 (2019-02-21 UTC)
No other RSOs were in this launch
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EGYPTSAT A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-22 03:34:50.140Z | 123.746° SE | 2025-10-22 03:37:50.140Z | 74.194° E | 25.743° | 2025-10-22 03:41:50.140Z | 10.199° NNE |
| 5 mins | 2025-10-22 05:12:50.140Z | 227.733° WSW | 2025-10-22 05:14:50.140Z | 266.142° W | 22.926° | 2025-10-22 05:17:50.140Z | 315.054° NNW |
| 6 mins | 2025-10-22 17:04:50.140Z | 23.105° NE | 2025-10-22 17:07:50.140Z | 143.769° SSE | 41.762° | 2025-10-22 17:10:50.140Z | 183.668° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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